Turbine Blades: Creep Resistant Materials and Design

Turbine Blades: Creep Resistant Materials and Design

[@muslimaly4053]

Excellent lecture I have ever seen! Hats off Sir ! Lots of love and respect from Pakistan

[@marktruong2803]

Great lecture! Appreciate and have an excellent health professor :)

[@ashokhosawad9027]

Thank you sir. It was excellent.

[@A.Lifecraft]

3:30 On tip clearance, i wonder if they could use a lip around the turbine front to produce a controlled separation of flow in the engine housing like they did on the SpaceShuttle main engine. With the flow separated from the housing, clearance would no longer matter that much... Or in other words, you create a Mach-diamond and put the turbine right in the middle of it.

[@death_parade]

Won't the varying throttle and airflow conditions of the engine lead to change in mach diamond position and size?

[@A.Lifecraft]

@@death_parade What i said was not to be taken literally. Yes, variations in flow would move the zone of maximum compression, still you would have useful tolerances, at least i guess so.

[@jisa98]

Nice class Professor, interesting topic.

[@raccoon_from_heaven]

20:43 "vinod taxi"

[@rajeshprasad101]

Thanks for point out. I should try to edit this out.

[@amiy24]

@@rajeshprasad101 no sir, everything was great. We loved your lecture.